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dc.contributor.otherTurbomachinery Symposium (42nd : 2013)
dc.creatorJustak, John
dc.date.accessioned2017-10-04T19:33:59Z
dc.date.available2017-10-04T19:33:59Z
dc.date.issued2013
dc.identifier.urihttp://hdl.handle.net/1969.1/162933
dc.descriptionCase Study
dc.description.abstractAn end user of a hydrogen compressor in an oil refinery application has identified existing labyrinth seals as a source of compressor inefficiency and a potential cause of rotor- dynamic instability. The objective of this effort was to investigate the applicability of a compliant/non-contacting seal developed for aerospace applications in the 5-stage hydrogen centrifugal compressor. This effort identified the potential seal performance of the compliant seals in the hydrogen compressor application 4 primary locations (shaft seal, impeller eye seal, thrust balance seal and barrier/buffer gas seal).
dc.format.mediumElectronic
dc.format.mimetypeapplication/pdf
dc.language.isoen
dc.publisherTexas A&M University. Turbomachinery Laboratories
dc.relation.ispartofProceedings of the 42nd Turbomachinery Symposium
dc.subject.lcshTurbomachines
dc.titleHydrogen Compressor Seal Case Study - Utilizing HALO (Non-Contacting, Compliant) Inter-Stage, Impeller Eye, Buffer and Fail-Safe Seals
dc.type.genrePresentation
dc.type.materialText
dc.identifier.doihttps://doi.org/10.21423/R1RP9D


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